Computational Parametric Study Of The Aerodynamics Of Spinning Slender Bodies At Supersonic Speeds
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Computational Parametric Study of the Aerodynamics of Spinning Slender Bodies at Supersonic Speeds
Three dimensional finite-difference flow field computation techniques have been employed to generate a parametric aerodynamic study at supersonic speeds. Computations for viscous turbulent and inviscid flow have been performed for cone-cylinder, secant-ogive-cylinder, and tangent-ogive-cylinder bodies for a Mach number range of 1.75